TY - JOUR
T1 - Liquid crystal device with reflective microstructure for attitude control
AU - Chujo, Toshihiro
AU - Ishida, Hirokazu
AU - Mori, Osamu
AU - Kawaguchi, Junichiro
N1 - Publisher Copyright:
Copyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2018/11/1
Y1 - 2018/11/1
N2 - Liquid crystal devices (LCDs) are proposedas fuel-free attitude control devices for spacecraft. The LCDs consist of multiple thin layers, including polymer-dispersed liquid crystal (PDLC) and a base film that has a microstructure with aluminum deposited onto it. When a voltage isapplied to anLCD, the crystalsinthe PDLC align with the electric field, and incident light passes through the PDLC layer and is reflected by the aluminum coating, whereas it is dispersed by randomly arranged crystals when no voltage is applied. This means that arrangements of LCDs can control both the magnitude and direction of reflection electrically, and they can achieve three-degree-of-freedom attitude control using solar radiation pressure. Because light diffracted by the layers causes optical interference, the PDLC has a polarization effect, and the microstructure shape has manufacturing errors, reflection from LCDs is a complex phenomenon and it must be understood to realize the desired performance." The first sentence all means the reason for the second sentence.
AB - Liquid crystal devices (LCDs) are proposedas fuel-free attitude control devices for spacecraft. The LCDs consist of multiple thin layers, including polymer-dispersed liquid crystal (PDLC) and a base film that has a microstructure with aluminum deposited onto it. When a voltage isapplied to anLCD, the crystalsinthe PDLC align with the electric field, and incident light passes through the PDLC layer and is reflected by the aluminum coating, whereas it is dispersed by randomly arranged crystals when no voltage is applied. This means that arrangements of LCDs can control both the magnitude and direction of reflection electrically, and they can achieve three-degree-of-freedom attitude control using solar radiation pressure. Because light diffracted by the layers causes optical interference, the PDLC has a polarization effect, and the microstructure shape has manufacturing errors, reflection from LCDs is a complex phenomenon and it must be understood to realize the desired performance." The first sentence all means the reason for the second sentence.
UR - http://www.scopus.com/inward/record.url?scp=85063234280&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85063234280&partnerID=8YFLogxK
U2 - 10.2514/1.A34165
DO - 10.2514/1.A34165
M3 - Article
AN - SCOPUS:85063234280
SN - 0022-4650
VL - 55
SP - 1509
EP - 1518
JO - Journal of Spacecraft and Rockets
JF - Journal of Spacecraft and Rockets
IS - 6
ER -